Experimental investigation of non-axisymmetric endwall profiling technique in cascades

被引：0
|
作者：
Wang, Chuanmei [1 ]
Li, Guojun [1 ]
Zheng, Jin [1 ]
Dong, Kangtian [2 ]
机构：
[1] School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China
[2] Fan Branch, Thermodynamics Power Research Institute, Xi'an 710032, China
来源：
Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University | 2008年 / 42卷 / 09期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1086 / 1090
相关论文
共 50 条
  • [31] NON-AXISYMMETRIC ENDWALL CONTOURING IN A COMPRESSOR CASCADE WITH TIP GAP
    Varpe, Mahesh K.
    Pradeep, A. M.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
  • [32] Design optimization of non-axisymmetric endwall contouring in compressor cascade
    Zhao, Wei-Guang
    Jin, Dong-Hai
    Gui, Xing-Min
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2013, 34 (06): : 1047 - 1050
  • [33] HEAT TRANSFER FOR A TURBINE BLADE WITH NON-AXISYMMETRIC ENDWALL CONTOURING
    Lynch, Stephen P.
    Sundaram, Narayan
    Thole, Karen A.
    Kohli, Atul
    Lehane, Christopher
    PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 3, PTS A AND B, 2009, : 887 - 898
  • [34] EFFECT OF NON-AXISYMMETRIC ENDWALL PROFILING ON HEAT TRANSFER AND FILM COOLING EFFECTIVENESS OF A TRANSONIC ROTOR BLADE
    Li, Jinjin
    Yan, Xin
    He, Kun
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5A, 2019,
  • [35] Aerodynamic Optimization of High Pressure Turbine Rotor Using Spline Surface Non-Axisymmetric Endwall Profiling
    Wang J.
    Wang Z.
    Ouyang Y.
    Tao Z.
    Song L.
    Li J.
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2024, 58 (03): : 38 - 48
  • [36] Effect of Non-Axisymmetric Endwall Profiling on Heat Transfer and Film Cooling Effectiveness of a Transonic Rotor Blade
    Li, Jinjin
    Yan, Xin
    He, Kun
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2020, 142 (05):
  • [37] ADVANCED NON-AXISYMMETRIC ENDWALL CONTOURING FOR AXIAL COMPRESSORS BY GENERATING AN AERODYNAMIC SEPARATOR - PART II: EXPERIMENTAL AND NUMERICAL CASCADE INVESTIGATION
    Hergt, Alexander
    Dorfner, Christian
    Steinert, Wolfgang
    Nicke, Eberhard
    Schreiber, Heinz-Adolf
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 121 - 131
  • [38] AUTOMATED OPTIMIZATION OF THE NON-AXISYMMETRIC HUB ENDWALL OF THE ROTOR OF AN AXIAL COMPRESSOR
    Reutter, Oliver
    Herve, Simon
    Nicke, Eberhard
    10TH EUROPEAN CONFERENCE ON TURBOMACHINERY: FLUID DYNAMICS AND THERMODYNAMICS, 2013,
  • [39] Effective strategy of non-axisymmetric endwall contouring in a linear compressor cascade
    Ma, Yuchen
    Teng, Jinfang
    Zhu, Mingmin
    Qiang, Xiaoqing
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (08) : 1473 - 1487
  • [40] THE APPLICATION OF NON-AXISYMMETRIC ENDWALL CONTOURING IN A SINGLE STAGE, ROTATING TURBINE
    Snedden, Glen
    Dunn, Dwain
    Ingram, Grant
    Gregory-Smith, David
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 831 - 840
12345